Missile azimuth alignment system

Details Missile azimuth alignment system Missile azimuth alignment system

1986-07-23

1987-07-21

Brown, David H.

Ordnance

Rocket launching

Having tubular guide means

89 1819, F41F 304

Patent

active

046810145

ABSTRACT:
A continuous alignment system for preventing rotation of a missile during on-loading in a launching tube, while permitting a controlled translation of the missile in the launching tube when subjected to external seismic shocks.

REFERENCES:
patent: 2448343 (1948-08-01), Zandmer
patent: 2998754 (1961-09-01), Bialy
patent: 3088374 (1963-05-01), Guyant et al.
patent: 3135162 (1964-06-01), Kamolian
patent: 3499364 (1970-03-01), D'Ooge
patent: 3899953 (1975-08-01), Labruyere
patent: 4155286 (1979-05-01), Mihm
patent: 4392411 (1983-07-01), Minkler
patent: 4415304 (1983-11-01), Tripoli et al.
patent: 4492143 (1985-01-01), Ruhle

Affiliated with

Also associated with

Rating

Missile azimuth alignment system does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Missile azimuth alignment system, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Missile azimuth alignment system will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-200988